JASC 2910
Service difficulty reports · 11,292
Reports filed under 2910 · Hydraulic System, Main, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2910' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2910' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA2013102800538Filter · failedFOUND NR 1 ENG EDP CASE DRAIN FILTER DPI POP OUT. REPLACED NR 1 ENG EDP CASE DRAIN FILTER LEAK CHECK CONDITION NORMAL.SDR CALA2013102992457Line · leakingHYD FLUID COMING DRAIN HOLE FWD OF RADAR ALT IN FRONT OF MAIN GEAR. FLUID COMING FROM BROKEN LINE, WHICH WAS REPAIRED, CLEANED UP LEAKING HYD FLUID.SDR DXTA2013102805547Line · leakingAFTER RETRACTING LANDING GEAR, RECEIVED AN AMBER CAS MESSAGE FOR HYDRAULIC VOLUME LOW. VOLUME GUAGE SHOWED ZERO. AFTER DOING CHECKLIST RECEIVED AMBER CAS MESSAGE HYD PRESSURE LOW LT & RT. REMOVED AND REPLACED FLEX HOSES TO NOSE WHEEL STEERING UNIT IAW MM 20SDR SWIA201335320Clamp · out of adjustLT MLG STRUT HYD LINE UPPER BAND CLAMP BOLT IS GOUGING GEAR DOOR. C-CHECK ADJUSTED UPPER BAND CLAMP ON LT MLG STRUT HYD LINE, REPAIRED & BLENDED DAMAGE IAW AMM & REO.SDR CALA2013103092510Hydraulic Line · leakingBELOW FWD CARGO PIT'S J-S DRIVE MOTOR, BILGE AREA, FOUND "DOOR CLOSE PRESS" HYD LINE FOAMING & DRIPPING AT SUPPORT CLAMP, YELLOW SYS. PERFORMED RYNLOCK REPAIR ON THE HYD LINE IAW GPM 1-0-13-028 & AMM 20-23-11-300-007A. INSTALLED REPAIRED HYD LINE, LEAK CHECKSDR CALA2013102992460Hydraulic Line · leakingEVIDENCE OF FLUID LEAK FROM VICINITY OF HYD SERVICE PANEL TO TAIL OF AIRCRAFT. BOTH LINES TO BRAKE VLV ON WW CEILING CENTERLINE LEAKING. TIGHTENED BOTH LINES NO LEAKS NOTED.SDR YENA20131025219Filter · unknownAIR RETURN, LANDING GEAR WOULD NOT COME UP. R & R NR 2 HYD SYS FILTER ELEMENTS & CASE DRAIN FILTER ELEMENT IAW AMM 29-11-07 & 29-11-05. LEAK CHECK GOOD. PERFORMED GEAR SWING 10 TIMES IAW AMM 32-33-00. OPS CHECK GOOD. RAN ENGINE & EDP PRESSURE GOOD. OK FOR SDR CA131030004O-Ring · failed(CAN) REF: DEFECT-1139169 LT ISO CL CAME ON, ON ROUTE. HYD QTY IN SYS 1 AFTER LANDING WAS 0.8. NR 1 NACELLE NR 1 HYDRAULICS. FLIGHT SPOILER PRESSURE SWITCH O-RING BLOWN, IPC REF 27-14-00 FIG 52 ITEM140. O-RING P/N-NAS1612-6A , REPLACED,LEAK AND FUNCTION CHSDR CALA2013102492347B-Nut · looseRAMP REPORTED AN OIL LEAK UNDER NR 2 ENG. OPENED COWL, TIGHTEN B-NUT ON ENG HYD PUMP LINE, MOTORED ENG. NO LEAKS NOTED DURING ENG MOTORING.SDR SIMA20131023007Filter · inoperativeCREW REPORTED DURING DESCENT, RECEIVED AN EICAS HYD 1 QTY MESSAGE. COMPLIED WITH AOM COL 1 PROCEDURES AND DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. TRANSFERED FLUID FROM SYS NR 2 TO SYSTEM NR 1 IAW ETN-EM-29-023. R & R THSDR AALA20131023003Module · inoperativeORD SYS B HYD PRESSURE FAILURE BOTH ENGINE & ELECTRIC PRESSURE LOSS. EMERGENCY DECLARED FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED SYSTEM B PRESSURE MODULE. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.SDR SIMA20131022003Line · leakingAFTER TAKEOFF, PILOTS AND F/A NOTICED STRONG ODOR THROUGHOUT THE CABIN AND COCKPIT. REPAIRED TWO HYD TUBES IN AFT FUSELAGE FS 925.00 - 1162.00 IAW 20-30-00. LEAK CHECKED GOOD. PERFORMED OPS CHECK OF AIR SYSTEM. NO DEFECTS NOTED. ACFT RETURNED TO SERVICE.SDR SIMA20131021005Hose · chafedCREW REPORTED DURING CRUISE, RECEIVED AN EICAS HYD 2, LOW QTY MESSAGE FOLLOWED BY ENG 2 HYD FAIL MESSAGE. COMPLIED WITH AOM VOL 1, PROCEDURES AND DECLARED AN EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. SERVICED HYD TO LEVELSDR SWIA201335043Drain · brokenBLUE HYDRAULIC SYSTEM NACELLE DRAIN IS CRACKED & BROKEN. C-CHECK REPLACED NACELLE DRAIN MASS ON RT OTBD NACELLE FOR BLUE HYDRAULIC SYSTEM IAW SRM.SDR SWIA201334979Hydraulic Line · failedON SHORT FINAL ALL OF HYD NR 2 FLUID QUANTITY WAS LOST WITH ASSOCIATED CAUTION MESSAGE. FLT 6227 REPLACED NR 2 ACMP PRESSURE LINE, NR 2 EDP, NR 2 RETURN FILTER ELEMENT, CASE DRAIN ELEMENT & THE PRESSURE MANIFOLD FILTER ELEMENT IAW AMM.SDR CALA2013102292247Hydraulic Line · leakingFOUND C-1 ACMP RETURN LINE LEAKING IN RT WHEEL APPROXIMATELY 30 DPM. INSTALLED TEMPERATURE HOSE ASSEMBLY FROM LINE KIT IAW GMM 1-0-13-003, OPERATIONS & LEAKS CHECKED GOOD.SDR AWKA201310220076Packing · leakingDURING INITIAL CLIMB, FLIGHT CREW NOTICED A SMOKE ODOR AND VISUALLY CONFIRMED SEEING A SMALL AMOUNT OF SMOKE IN CABIN. ELECTED TO DECLARE AN EMERGENCY AND RETURN TO FIELD. DURING DOWNWIND FOR THE RUNWAY, SMOKE DISSIPATED. MADE AN UNEVENTFUL LANDING AND TAXIESDR CA131023004Check Valve · failed(CAN) DURING ROUTINE C-CHECK MAINTENANCE THE BLUE HYDRAULIC SYS CHECK VALVE, PN 2050 GM FAILED. THE FAILURE WAS INTERNAL TO THE CHECK VALVE. CHECK VALVE REPLACED.SDR PCSA2013102201Hose · rupturedCENTER HYD SYSTEM FLUID QUANTITY LOSS, FRM CODE 29-90-11-43.SDR SIMA20131017009Hydraulic System · contaminatedOTBD FLT SPOILERS CAUTION MESSAGE. BLED HYD SYS 1 IAW AMM 29-10-00. REMOVED AIR FROM SYSTEM. SERVICED NR 1 HYD SYS IAW AMM 12-12-29. PERFORMED POST 2 TEST IAW AMM 27-61-05. OPS NORMAL.SDR FDEA201310172539Selector · leakingENROUTE, GREEN SYS FLUID IN RESEVOIR DECREASED TO RED DOT ECAM PROCEDURES. PUMPS TURNED OFF AND NR 6 SPOILER. GRAVITY EXTENDED GEAR. R & R THE GREEN SYS MANIFOLD SERVO CONTROL MODULE IN REF TO AMM 29-11-34-04 AND R & R SERVO CONTROL SELECTOR VALVE IAW AMM 2SDR CA131018009Housing · damaged(CAN) DURING TROUBLESHOOTING OF A L/E FLAP/SLAT DEFECT, UPON CYCLING FLAPS UP & DOWN HYD SYSTEM "A" MODULE CHECK VALVE FAILED, THREADED CHECK VALVE DEPARTED THE HOUSING BODY, THREADS PULLED FROM HOUSING BODY. SYSTEM A MODULE REPLACED, ALL SYSTEMS CHECKED NORSDR F3LA2013101800924Line · leakingHYD YELLOW LOW PRESSURE. R & R CRACKED HCU LINE FROM TRSOV. NO LEAKAGE NOTED REF AMM 29-13-19-400-049.SDR SWAA2013102821479Fitting · cracked"B" SYSTEM HYDRAULIC QUANTITY AT REFILL, FOUND HYDRAULIC LEAK RT WW CEILING AFT. FOUR WAY HYDRAULIC CROSS FITTING CRACKED. R & R FITTING IAW SIP.SDR JIKA2013101800001Line · leakingON REACHING CRUISE ALTITUDE OF 21,000 FT, WITHIN FIVE MINUTES, RIGHT HYDRAULIC FAIL ANNUNCIATOR ILLUMINATED. OPENED QUICK REF HANDBOOK TO FIND APPLICABLE ITEMS THAT MIGHT HELP ISOLATE AND DETERMINE PROBLEM. DIVERTED. IN 2 MINUTES, HYD PRESSURE WENT TO ZERSDR CALA2013101592069B-Nut · looseSLOW LEAK COMING FROM BOTTOM OF WING JUST FWD OF RT MAIN GEAR STRUT. FOUND B NUT LOOSE. FASTENED, OK TO CONTINUE.SDR USAA2013101500002Pressure Switch · faultyIN CLIMB, ECAM MESSAGE HYD G ENG 1 PUMP LO PRESSURE. R & R ENGINE HYD PRESSURE SWITCH IAW AMM 29-11-17-400-010-A.SDR CALA2013101091947Hydraulic Line · leakingHYD LEAK FROM "UP 2" PRESS LINE APPROXIMATELY 4 FEET FROM GROUND SPEED BRAKE VLV UNDER CLAMP. REMOVED LINE IAW IPC 27-61-67-001 ITEM 305. ACCOMPLISHED RYNGLOK REPAIR IAW GNMM 1-0-13-028. NEED TO LEAK CHECK LINE WITH HYD PRESS. LINE LOCATED IN RT WLG WW. CSDR CHQA20131009367Line · cutCREW REPORTED THAT THEY RECEIVED A HYD SYS LOW QUANTITY MESSAGE FOLLOWED BY AN ENGINE 1 HYD PUMP FAIL MESSAGE ON DESCENT. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE PRESSURE LINE ON THE NR 1 HYD PUMP. OPS AND SDR AALA20131009001Check Valve · inoperativeLAX CREW REPORTED NR 2 ENG HYD PUMP LOW PRESSURE LIGHT ILLUMINATED. EMERGENCY DECLARED FLIGHT RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED ENG DRIVEN PUMP THAT HAD SEIZED & RT HAND CASE DRAIN CHECK VALVE. SYSTEM GROUND CHESDR CALA2013100891846Fluid · leakingFLUID UNDER RT HORIZONTAL STAB & UNDER FUSELAGE. REMOVED PANEL TO CHECK PCU'S. OPERATED ALL THREE SYSTEMS & OPERATED ELEVATOR SEVERAL TIMES, NO ACTIVE LEAKS FOUND. ALL HYDRAULIC QTYS OKSDR CALA2013100891845B-Nut · looseHYDRAULIC LEAK EVIDENCE UNDER RT WING RT AILERON. ACCOMPLISHED OPERATIONAL CHECK OF RT AILERON SYSTEM. TIGHTENED AILERON B-NUT UNIONS, NO LEAKS NOTED IAW AMM-29-00-99.SDR CA131007027Cylinder · cracked(CAN) NR 2 HYDRAULIC SYSTEM WAS LEAKING HYDRAULIC FLUID. LEAK WAS FOUND TO BE COMING FROM THE RT MLG AFT/CENTER DOOR ACTUATOR. THE ACTUATOR WAS REPLACED AND ACFT RETURNED TO SERVICE. VISUALLY INDENTIFIED FLUID SEEPING FROM THE ACTUATOR CYLINDER HOUSING BELOSDR CALA2013100791762Hydraulic Line · frayedRT TRUCK TILT ACTUATOR LINE FRAYED. REPAIRED COVERING IAW GNMM 1-0-13-008.SDR CALA2013100491735Fluid · leakingHYD FLUID LEAKING ON TOP OF TAIL CONE FROM RUDDER DRAIN, FOUND ON WALK AROUND.SDR CA131007019Tube · leaking(CAN) HYDRAULIC GREEN SYSTEM LEAK DETECTED BY ECAM IN FLIGHT, FLUID QTY DECREASING. QRH PROCEDURES WAS CARRIED OUT AND ENGINE DRIVEN HYDRAULIC PUMP WAS SELECTED OFF FOR THE REMAINDER OF THE FLIGHT. ACFT LANDING WAS UNEVENTFUL AND ACFT TOWED OFF THE RUNWAY DUESDR CA131004005Check Valve · fractured(CAN) SHORTLY AFTER TAKEOFF, FLIGHT CREW RECEIVED A NR 2 HYD ISO VALVE CAUTION MESSAGE AND NOTICED THAT THE HYDRAULIC NR 2 SYSTEM FLUID LEVEL HAD DEPLETED TO 0.5. INBOUND OF THE DESTINATION AIRPORT AN EMERGENCY WAS DECLARED AND AN ALTERNATE LANDING GEAR EXTENSSDR SWAA2013100720842Hydraulic Line · leakingAIR TURN BACK AFTER TAKEOFF WITH GEAR HANDLE UP RED LIGHT REMAINED ON IN NOSE GEAR INDICATOR WHEN HANDLE MOVED TO OFF NOSE GEAR FELL DOWN. R & R LOCK ACTUATOR PRESSURE LINE IAW MM.SDR CALA2013100491752Hydraulic Line · damagedENGINE DRIVEN PUMP HYDRAULIC POWER. POSITION 2O1=L,O2=R, ENGINE DRIVEN PUMP HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. EICAS MESSAGE DISPLAYED LT, RT HYDRAULIC PRIM PUMP. EICAS MESSAGE LT,RT HYDRAULIC SYSTEM MAINTENANCE WAS, WAS NOT DISPLAYED. IAW LOG1 & SMSDR CALA2013100491740O-Ring · damagedHYDRAULIC LEAK NOTED ON WALK AROUND NEAR RT WW. FOUND O-RING LEAKING IN YELLOW SYSTEM HYDRAULIC BAY, REPLACED & LEAK CHECKED GOOD.SDR SWIA201335054Support Frame · crackedRT HYDRAULIC PACK LOWER SUPPORT FRAME CRACKED. C-CHECK REPLACED RT HYDRAULIC PACK LOWER SUPPORT FRAME & SECURED IAW SRM.SDR FDEA201310022367Line · leakingDURING CRUISE, ECAM INDICATED LOSS OF GREEN SYS FLUID. OVERHEAD & ECAM CONFIRMED SAME ISSUE. PERFORMED QRH PROCEDURE & DIVERTED. EMERGENCY DECLARED. NR 1 ENGINE HAS RUNNING HYD LEAK. FOUND GREEN SYS EDP PRESSURE LINE CHAFED AND LEAKING. REMOVED AND REPSDR FDEA201310022378Hose · leakingABOUT 45-50 MINUTES AFTER TAKE OFF, RECEIVED AN ECAM WARNING, HYD GREEN RESERVOIR LOW LEVEL INDICATION ON OVERHEAD PANEL AND RT ECAM WERE ALMOST ZERO. COMPLIED WITH ECAM AND QRH. R & R NR 2 ENGINE GREEN SYSTEM HYD PRESSURE LINE REF SMP & MM 29-11-32-04-02. SDR SWAA2013100921046Module · faultyWITH FLAPS 0-15 WE NOTICED THE AILERONS BINDING. WITH THE AUTOPILOT ENGAGED THE AUTOPILOT WOULD NOT ROLL MORE THAN 10 DEGREES WHEN THE LOC CAPTURED. THE AUTOPILOT ROLL MODE WAS DISCONNECTED WITH THE ROLL MODE IN CLOCKWISE THE AILERONS WERE BINDING AIRSPEED WSDR CALA2013093091554Bolt · looseRAMP REPORT AT DEPARTURE LEAK AT LT MAIN GEAR WW DOOR. FOUND DRIP LEAK BRAKE HYD PACKAGE PARTING SURFACE LOCATED ON AFT LT WING SPAR. TIGHTENED MOUNT BOLTS LEAKAGE CEASED.SDR SIMA20130928004Hose · leakingTHE CREW REPORTED DURING DESCENT A HYD 2 LOW PRESSURE CAUTION MESSAGE. COMPLIED WITH AOM VOL 1 PROCEDURES AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R RT HYD DAMPENER HOSE IAW AMM 29-11-59. LEAK AND OPS CHECKED GOOD.SDR A8JA201309280017Clamp · looseDURING CLIMB, EXPERIENCED RED LANDING GEAR DISAGREEMENT LIGHT. DID NOT NOTICE OR HEAR ANY OTHER FACTORS TO ALARM THEM OF ANY MECHANICAL FAILURES. CONTINUED TO DESTINATION. DURING FINAL APPROACH, EXTENDED LANDING GEAR AND RED LIGHT EXTINGUISHED AND ALL THRSDR CALA2013093091560Hydraulic Line · chafedHYD LEAK FROM LT OTBD AILERON. HYD TUBE TO LT OTBD AILERON ACT CHAFED BY A OTBD AILERON ACT SAFETY WIRE. TUBE IPC 27-11-73-01 ITEM 590 REPLACE PN 272T1200-101, LEAK CHECKED IAW AMM 27 11 49 PERF NO LEAK.SDR CA131002008O-Ring · leaking(CAN) HYDRAULIC SYSTEM PUMP, FLAPS & GEARS, IN CLIMB, GEARS DOWN WITH EMERGENCY HANDLE. POWER PACK FOUND EMPTY, LEAK BY LT EMERGENCY VALVE, REPLACED O-RING M97E775-112, SYSTEM SERVICED AND TESTED, LEAK CHECKED. OK, RETRACTION CARRIED OUT AND OK.SDR CALA2013092491391Circuit Card · failedHYDRAULIC PUMP EICAS MESSAGE DISPLAYED. REPLACED HYD IM CARD IAW AMM, MESSAGE CLEARED.
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